Technical Drawing

Thunder 12~24S 200A High Power UAVs ESC
T8542 F3P 4D Airplane Polymer Propeller
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| KV | 65 | Motor size | φ144.2*78.1mm |
| Shaft Diameter | IN20 OUT12 | Motor Weight(Incl. Cable) | 1680g |
| Idle Current (20V) | 3A | Configuration | 42N38P |
| Internal Resistance | 26±2mΩ | Lead Spec | Enamelled wire straight out 150mm |
| Ingress ProtectionLevel | IPX5 | Rated Voltage (Lipo) | 24S,Max. 104V |
| Peak Current (15s) | 190A | Propeller Recommendation | VZ42*16.5” |
| Max. Continuous Power | 6000W | ESC Recommendation | THUNDER 200A 24S |
| Type | Voltage (V) | Propeller | Throttle | Thrust (g) | Torque (N*m) | Current (A) | RPM | Power (W) | Efficiency (g/W) | Operating Temperature (℃) |
V13L KV65 | 100V | VZ42*16.5” | 30% | 10673 | 5.28 | 14.20 | 1920 | 1416 | 7.5 | HOT |
| 35% | 15011 | 7.27 | 22.06 | 2280 | 2185 | 6.9 | ||||
| 40% | 20478 | 9.79 | 34.24 | 2610 | 3390 | 6.0 | ||||
| 45% | 26640 | 12.69 | 49.93 | 2970 | 4926 | 5.4 | ||||
| 50% | 30648 | 14.56 | 61.22 | 3150 | 6020 | 5.1 | ||||
| 55% | 37024 | 17.62 | 83.95 | 3450 | 8194 | 4.5 | ||||
| 60% | 41902 | 19.93 | 104.33 | 3690 | 10175 | 4.1 | ||||
| 65% | 44101 | 21.01 | 113.65 | 3780 | 11053 | 4.0 | ||||
| 70% | 46184 | 22.05 | 123.56 | 3870 | 11925 | 3.9 | ||||
| 75% | 48383 | 23.08 | 135.21 | 3960 | 13038 | 3.7 | ||||
| 80% | 50260 | 24.02 | 147.27 | 4050 | 14156 | 3.6 | ||||
| 85% | 52410 | 24.99 | 160.68 | 4140 | 15433 | 3.4 | ||||
| 90% | 54056 | 25.87 | 175.08 | 4200 | 16699 | 3.2 | ||||
| 95% | 55454 | 26.51 | 194.05 | 4230 | 18382 | 3.0 | ||||
| 100% | 54754 | 26.18 | 195.81 | 4230 | 18563 | 2.9 | ||||
| Note: Motor temperature is motor surface temperature at 75% throttle running 30s. (Date above based on benchtest are for reference only, comparion with that of other motor types is not recommended.) | ||||||||||
